Vortex-motion

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• Fluid dynamics
• Rotational motion
• Hydrodynamics
• Eddies
• Aerodynamics

• Vortex-motion -- Computer simulation
• Vortex-motion -- Mathematical models
• Vortex-motion -- Mathematics
• Vortex-motion -- Measurement
• Vortex-motion -- Remote sensing
• Vortex-motion -- Testing
• Acoustic streaming
• Vortex generators
• Vortex tubes
• Wakes (Fluid dynamics)
• Whirlpools
• Whirlwinds

• Elements of the mathematical theory of fluid motion; Wave and vortex motion. By Thomas Craig. (New York, D. Van Nostrand, 1879), by Thomas Craig (page images at HathiTrust)
• Thʹeorie des tourbillons. Leçons professʹees pendant le deuxième semestre 1891-92, par H. Poincarʹe. Rédigées par M. Lamotte. (Paris, G. Carrʹe, 1893), by Henri Poincaré (page images at HathiTrust; US access only)
• De wervelbeweging.... door Jan Cornelis van den Berg ... (Haarlem, De Haarlemsche boek- en muziekhandel, 1888), by Jan Cornelis van den Berg (page images at HathiTrust; US access only)
• Vortical cloud patterns on the leeward side of islands / by Lu Ting (Washington, D.C. : Polytechnic Institute of Brooklyn, Dept. of Aerospace Engineering and Applied Mechanics ; prepared for U.S. Weather Bureau, 1963), by Lu Ting (page images at HathiTrust)
• Ueber die Entstehung und Fortbewegung des Wirbelpaares hinter zylindrischen Körpen. (Göttingen, 1914), by Hans Ludwig Rubach (page images at HathiTrust; US access only)
• Solids separation by a hydraulic cyclone with a batch underflow receiver / P.A. Haas. (Oak Ridge, Tenn. : Oak Ridge National Laboratory, 1960), by P. A. Haas (page images at HathiTrust)
• Théorie des tourbillons. Leçons professées pendant le deuxième semestre 1891-92, par H. Poincaré... (Paris, G. Carré, 1893), by Henri Poincaré (page images at HathiTrust; US access only)
• Studier öfver elastika rotationskroppars deformation. (Upsala, 1896), by Olof Josephson (page images at HathiTrust; US access only)
• On the dynamics of the circular vortex : with applications to the atmosphere and atmospheric vortex and wave motions / by V. Bjerknes. (Kristiana (Oslo), Norway : Grøndahl & Søns Boktrykkeri, 1921), by V. Bjerknes (page images at HathiTrust; US access only)
• Theory of the lifting airscrew = Teoriya nesushchego vinta / V. E. Baskin ... [et. al.] ; edited by A. K. Martynov ; translated by W. Z. Stepniewski ; transcribed by W. L. Metz. (Washington : U.S. National Aeronautics and Space Administration ; Springfield, Va. : for sale by the National Technical Information Service, 1976) (page images at HathiTrust)
• Wind-tunnel free-flight investigation of a 0.15-scale model of the F-106B airplane with vortex flaps / Long P. Yip. (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Office ; Springfield, Va. : For sale by the National Technical Information Service, 1987), by Long P. Yip (page images at HathiTrust)
• Evaluation of installed performance of a wing-tip-mounted pusher turboprop on a semispan wing / James C. Patterson, Jr., and Glynn R. Bartlett. (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Office ; Springfield, Va. : For sale by the National Technical Information Service, 1987), by James C. Patterson (page images at HathiTrust)
• Piloted-simulation study of effects of vortex flaps on low-speed handling qualities of a delta-wing airplane / Jay M. Brandon and Philip W. Brown, Alfred J. Wunschel. (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Office ; Springfield, Va. : For sale by the National Technical Information Service, 1987), by Jay M. Brandon (page images at HathiTrust)
• Measurement of velocity and vorticity fields in the wake of an airfoil in periodic pitching motion / Earl R. Booth, Jr. (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Division ; Springfield, Va. : For sale by the National Technical Information Service, 1987), by Earl R. Booth (page images at HathiTrust)
• Transonic and supersonic Euler computations of vortex-dominated flow fields about a generic fighter / Aga M. Goodsell and John E. Melton. (Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1991), by Aga M. Goodsell (page images at HathiTrust)
• Wind tunnel investigation of vortex flows on F/A-18 configuration at subsonic through transonic speeds / Gary E. Erickson. (Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1991), by Gary E. Erickson (page images at HathiTrust)
• Flow field over the wing of a delta-wing fighter model with vortex control devices at Mach 0.6 to 1.2 / E. Ann Bare and David E. Reubush, Raymond C. Haddad. (Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992), by E. Ann Bare (page images at HathiTrust)
• Water-tunnel experiments on an oscillating airfoil at RE = 21,000 / Kenneth W. McAlister and Lawrence W. Carr. ([Washington] : National Aeronautics and Space Administration, Scientific and Technical Information Office ; Springfield, Va. : For sale by the National Technical Information Service, 1978), by Kenneth W. McAlister (page images at HathiTrust)
• Lee-side flow over delta wings at supersonic speeds / David S. Miller and Richard M. Wood. (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; Springfield, Va. : For sale by the National Technical Information Service, 1985), by David S. Miller (page images at HathiTrust)
• A cockpit-display concept for executing a multiple glide-slope approach for wake-vortex avoidance / Terence S. Abbott. (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; Springfield, Va. : For sale by the National Technical Information Service, 1985), by Terence S. Abbott (page images at HathiTrust)
• New technique for experimental generation of two-dimensional blade-vortex interaction at low Reynolds numbers / Earl R. Booth, Jr., and James C. Yu. (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; Springfield, Va. : For sale by the National Technical Information Service, 1986), by Earl R. Booth (page images at HathiTrust)
• Exploratory wind-tunnel investigation of a wingtip-mounted vortex turbine for vortex energy recovery / James C. Patterson, Jr., and Stuart G. Flechner. (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; Springfield, Va. : For sale by the National Technical Information Service, 1985), by James C. Patterson (page images at HathiTrust)
• Vortex wake alleviation studies with a variable twist wing G. Thomas Holbrook, Dana Morris Dunham, and George C. Greene. ([Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1985), by G. Thomas Holbrook (page images at HathiTrust)
• Low-speed wind-tunnel investigation of forward-located spoilers and trailing splines as trailing-vortex hazard-alleviation devices on an aspect-ratio-8 wing model / Delwin R. Croom. (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1975), by Delwin R. Croom (page images at HathiTrust)
• A distributed vortex method for computing the vortex field of a missile / Raymond L. Barger. ([Washington] : National Aeronautics and Space Administration, Scientific and Technical Information Office ; Springfield, Va. : For sale by the National Technical Information Service, 1978), by Raymond L. Barger (page images at HathiTrust)
• Water-tunnel investigation of concepts for alleviation of adverse inlet spillage interactions with external stores / Dan H. Neuhart, Matthew N. Rhode. (Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; Springfield, Va. : For sale by the National Technical Information Service, 1990), by Dan H. Neuhart (page images at HathiTrust)
• Effect of inlet ingestion of a wing tip vortex on compressor face flow and turbojet stall margin / Glenn A. Mitchell. (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1975), by Glenn A. Mitchell (page images at HathiTrust)
• Semiempirical method for predicting vortex-induced rolling moments / Dennis O. Allison and Percy J. Bobbitt. (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; Springfield, Va. : For sale by the National Technical Information Service, 1985), by Dennis O. Allison (page images at HathiTrust)
• In-flight flow visualization characteristics of the NASA F-18 high alpha research vehicle at high angles of attack / David F. Fisher and John H. Del Frate, David M. Richwine. (Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; Springfield, VA : For sale by the National Technical Information Service, 1990), by David F. Fisher (page images at HathiTrust)
• Low-speed wind-tunnel parametric investigation of flight spoilers as trailing-vortex-alleviation devices on a transport aircraft model / Delwin R. Croom. (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Office ; [Springfield, Va. : For sale by the National Technical Information Service], 1979), by Delwin R. Croom (page images at HathiTrust)
• Design and preliminary tests of a blade tip air mass injection system for vortex modification and possible noise reduction on a full-scale helicopter rotor / Robert J. Pegg ... [et al.]. (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1975) (page images at HathiTrust)
• Experimental and analytical study of the longitudinal aerodynamic characteristics of analytically and empirically designed strake-wing confirurations at subcritical speeds / John E. Lamar and Neal T. Frink. (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1981), by John E. Lamar (page images at HathiTrust)
• Effects of fog droplets on wake vortex decay rate / T.H. Moulden and Walter Frost ; prepared by University of Tennessee Space Institute, Tullahoma, Tenn., for George C. Marshall Space Flight Center. (Washington : National Aeronautics and Space Administration ;, 1976), by Trevor H. Moulden (page images at HathiTrust)
• Experiments on confined turbulent jets in cross flow / by Yasuhiro Kamotani and Isaac Greber. (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service, 1974]), by Yasuhiro Kamotani (page images at HathiTrust)
• Vortex interactions and decay in aircraft wakes / Alan J. Bilanin ... [et al.]. (Washington : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service, 1977) (page images at HathiTrust)
• An experimental study of rotor blade-vortex interaction / by Makam Surendraiah. (Washington, D.C. : National Aeronautics and Space Administration, 1970), by Makam Surendraiah (page images at HathiTrust)
• Analytical studies of separated vortex flow on highly swept wings / John M. Kuhlman, Old Dominion University Research Foundation ; prepared for Langley Research Center. ([Washington] : National Aeronautics and Space Administration, Scientific and Technical Information Office ; Springfield, Va. : For sale by the National Technical Information Service, 1978), by John M. Kuhlman (page images at HathiTrust)
• A method for computing the leading-edge suction in a higher-order panel method / F. Edward Ehlers and Marjorie E. Manro ; prepared for Langley Research Center. (Washington, D.C. : National Aeronautical and Space Administration, Scientific and Technical Information Office ; [Springfield, Va. : For sale by the National Technical Information Service], 1984), by F. Edward Ehlers (page images at HathiTrust)
• Calculation of symmetric and asymmetric vortex separation on cones and tangent ogives based on discrete vortex models / by S. Chin and C. Edward Lan. (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Division, 1988), by S. Chin (page images at HathiTrust)
• The vortex structure of the cloud cover according to weather satellite data / by L.S. Minina. ([Washington, D.C.] : National Aeronautics and Space Administration, [1964]), by Li͡udmila Silʹvestrovna Minina (page images at HathiTrust)
• The lateral-directional characteristics of a 74-degree delta wing employing gothic planform vortex flaps / Arthur C. Grantz. (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; Springfield, Va. : For sale by the National Technical Information Service, 1984), by Arthur C. Grantz (page images at HathiTrust)
• Characteristics of wake vortex generated by a Boeing 727 jet transport during two-segment and normal ILS approach flight paths / R.L. Kurkowski, M.R. Barber, and L.J. Garodz ; Ames Research Center, Moffett Field, Calif. (Washington : U.S. National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service, 1976), by R. L. Kurkowski (page images at HathiTrust)
• An experimental investigation of the velocity fluctuations behind oscillating vanes / by Doanld A. Buell. (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the Clearinghouse for Federal Scientific and Technical Information, 1969]), by Donald A. Buell (page images at HathiTrust)
• Exploratory flight investigation of aircraft response to the wing vortex wake generated by jet transport aircraft / William H. Andrews, Glenn H. Robinson, and Richard R. Larson. (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1972), by William H. Andrews (page images at HathiTrust)
• An exploratory wind-tunnel investigation of the wake effect of a panel tip-mounted fan-jet engine on the lift-induced vortex / James C. Patterson, Jr., and Stuart G. Flechner. (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; Springfield, Va. : For sale by the National Technical Information Service, 1970), by James C. Patterson (page images at HathiTrust)
• Charts for predicting the subsonic vortex-lift characteristics of arrow, delta, and diamond wings / by Edward C. Polhamus. (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1971), by Edward C. Polhamus (page images at HathiTrust)
• Low-speed wind-tunnel investigation of flight spoilers as trailing-vortex-alleviation devices on a medium-range wide-body tri-jet airplane model / Delwin R. Croom, Raymond D. Vogler, and Geoffrey M. Williams. (Washington : National Aeronautics and Space Administration : Springfield, Va. : For sale by the National Technical Information Service, 1976), by Delwin R. Croom (page images at HathiTrust)
• Effects of wing leading-edge radius and Reynolds number on longitudinal aerodynamic characteristics of highly swept wing-body configurations at subsonic speeds / William P. Henderson ; Langley Research Center. (Washington : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service, 1976), by William P. Henderson (page images at HathiTrust)
• Low-speed wind-tunnel investigation of flight spoilers as trailing-vortex-alleviation devices on an extended-range wide-body tri-jet airplane model / Delwin R. Croom, Raymond D. Vogler, and John A. Thelander ; Langley Research Center. (Washington : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service, 1976), by Delwin R. Croom (page images at HathiTrust)
• Examination of the solutions of the Navier-Stokes equations for a class of three-dimensional vortices, by Coleman duP. Donaldson and Roger D. Sullivan. Prepared for Air Force Office of Scientific Research, Air Research and Development Command, U. S. Air Force. (Princeton, N. J., Aeronautical Research Associates of Princeton, Inc., 1960-), by Coleman DuPont Donaldson (page images at HathiTrust)
• A treatise on the motion of vortex rings. An essay to which the Adams prize was adjudged in 1882, in the University of Cambridge. (London, Macmillan and co., 1883), by J. J. Thomson (page images at HathiTrust)
• Die Helmholtzsche Wirbeltheorie für Ingenieure bearbeitet von Dr. phil. Dr. Ing. H. C. G. Bauer. Mit 58 Textabbildungen. (München, Berlin, R. Oldenbourg, 1919), by G. Bauer (page images at HathiTrust; US access only)

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